View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 14974U 84046B 22145.20778691 .00000058 00000-0 43486-4 0 9993
2 14974 82.9372 240.8698 0044850 357.1423 65.9962 13.76938539910080
Epoch (UTC): | 25 May 2022 04:59:12 |
Eccentricity: | 0.0044850 |
inclination: | 82.9372° |
perigee height: | 942 km |
apogee height: | 1008 km |
right ascension of ascending node: | 240.8698° |
argument of perigee: | 357.1423° |
revolutions per day: | 13.76938539 |
mean anomaly at epoch: | 65.9962° |
orbit number at epoch: | 91008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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